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- W2106585606 abstract "The effect of stream-wise fences on the twin-tail buffet responses of generic fighter aircraft is presented. The generic fighter aircraft consists of a sharp-edged delta wing of aspect ratio one and swept-back, flexible, vertical twin tail of taper ratio of 0.23. Twin streamwise fences are located at the 30% chord-station of the delta wing. The fences are used to alter the vortical flow and vortex breakdown location above the delta wing in order to alleviate the twin-tail buffet. The effect of the geometrical shape of the fences and the performance of the fences over wide range of angles of attack are investigated. This complex multi-disciplinary problem is solved using the multi-disciplinary computing environment (MDICE). The results indicated that the fences are effective in reducing the aeroelastic loads and responses, especially at angles of attack less than 30°. The fences of taper ratio of 0.7 produced the most favorable results." @default.
- W2106585606 created "2016-06-24" @default.
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- W2106585606 date "2000-08-14" @default.
- W2106585606 modified "2023-09-28" @default.
- W2106585606 title "Effect of stream-wise fences on twin-tail buffet responses" @default.
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- W2106585606 doi "https://doi.org/10.2514/6.2000-4410" @default.
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